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Bayonet for superfluid helium transfer in spaceA prototype superfluid helium bayonet for potential space applications has been developed and evaluated with a low heat leak test apparatus. Measured heat leak of the 13 mm (1/2 inch) bayonet pair is 0.21 W at 1.8 K with an uncertainty of +0.09/-0.05 W. Bayonets are fabricated with thin, electron beam (EB) welded tubes which are EB welded to machined nose and flange pieces. Low heat leak structural integrity is provided by a 0.9 mm thickness of filament wound fiberglass-epoxy. Superfluid creep is restricted by KEL-F nose seals which form vacuum-tight extensions to the bayonet cold end pieces.
Document ID
19880065993
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mcintosh, G. E.
(Cryolab, Inc. San Luis Obispo, CA, United States)
Lombard, D. S.
(Cryolab, Inc. San Luis Obispo, CA, United States)
Martindale, D. L.
(Cryolab, Inc. San Luis Obispo, CA, United States)
Dipirro, Michael J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Astronautics (General)
Meeting Information
Meeting: Advances in cryogenic engineering.
Location: Saint Charles, IL
Country: United States
Start Date: June 14, 1987
End Date: June 18, 1987
Accession Number
88A53220
Funding Number(s)
CONTRACT_GRANT: NAS5-29224
Distribution Limits
Public
Copyright
Other

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